CN108216578B - 飞行器的机翼 - Google Patents

飞行器的机翼 Download PDF

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Publication number
CN108216578B
CN108216578B CN201711285195.9A CN201711285195A CN108216578B CN 108216578 B CN108216578 B CN 108216578B CN 201711285195 A CN201711285195 A CN 201711285195A CN 108216578 B CN108216578 B CN 108216578B
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CN
China
Prior art keywords
slat
hinge
track
wing
connection assembly
Prior art date
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Active
Application number
CN201711285195.9A
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English (en)
Chinese (zh)
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CN108216578A (zh
Inventor
洛伦斯·弗洛里安
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Airbus Operations GmbH
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Airbus Operations GmbH
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Publication date
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Publication of CN108216578A publication Critical patent/CN108216578A/zh
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Publication of CN108216578B publication Critical patent/CN108216578B/zh
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/34—Transmitting means without power amplification or where power amplification is irrelevant mechanical using toothed gearing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
CN201711285195.9A 2016-12-22 2017-12-07 飞行器的机翼 Active CN108216578B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP16206500.7A EP3339163A1 (fr) 2016-12-22 2016-12-22 Aile d'avion
EP16206500.7 2016-12-22

Publications (2)

Publication Number Publication Date
CN108216578A CN108216578A (zh) 2018-06-29
CN108216578B true CN108216578B (zh) 2022-02-01

Family

ID=57590404

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711285195.9A Active CN108216578B (zh) 2016-12-22 2017-12-07 飞行器的机翼

Country Status (3)

Country Link
US (1) US11021229B2 (fr)
EP (1) EP3339163A1 (fr)
CN (1) CN108216578B (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3339163A1 (fr) * 2016-12-22 2018-06-27 Airbus Operations GmbH Aile d'avion
ES2878314T3 (es) 2017-04-26 2021-11-18 Asco Ind Nv Conjunto de guía para una pista portadora del dispositivo hipersustentador del borde delantero aerodinámico
ES2886667T3 (es) 2017-12-19 2021-12-20 Asco Ind Nv Sistema de despliegue para un dispositivo de borde de ataque de sustentación elevada de perfil aerodinámico
CN109367761B (zh) * 2018-10-11 2022-05-31 西北工业大学 一种用于旋转机翼的襟翼收放操纵机构

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CN101450712A (zh) * 2007-12-06 2009-06-10 滚动轴承美国公司 用于升力辅助装置的致动系统和其中使用的滚子轴承
CN101466597A (zh) * 2006-06-14 2009-06-24 波音公司 用于有间隙刚性克鲁格襟翼的连杆机构及相关系统和方法
EP2272752A2 (fr) * 2009-07-07 2011-01-12 Goodrich Actuation Systems Limited Agencement d'actionneur
CN102834315A (zh) * 2010-03-31 2012-12-19 波音公司 带有可展开机翼前缘元件的低噪音机翼缝翼系统
CN103448906A (zh) * 2012-05-31 2013-12-18 空中客车营运有限公司 缝翼支撑组件
CN104039647A (zh) * 2011-06-28 2014-09-10 空中客车运作有限责任公司 具有主翼和增升体的机翼及实现调节增升体相对于主翼的运动的方法

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FR1395340A (fr) * 1964-05-19 1965-04-09 British Aircraft Corp Ltd Perfectionnements aux dispositifs hyper-sustentateurs pour avions
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
US4470569A (en) * 1981-12-28 1984-09-11 Mcdonnell Douglas Corporation Locking, redundant slat drive mechanism
US5927656A (en) * 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
US6598834B2 (en) * 2000-02-14 2003-07-29 Aerotech Services Inc. Method for reducing fuel consumption in aircraft
DE10019185C2 (de) * 2000-04-17 2003-06-05 Airbus Gmbh Anordnung zur aerodynamischen Lärmminderung von Vorflügeln eines Verkehrsflugzeuges
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
DE10133920B4 (de) * 2001-07-12 2004-05-13 Eads Deutschland Gmbh Auftriebsklappen-Mechanismus
DE10157849A1 (de) * 2001-11-24 2003-06-12 Airbus Gmbh Anordnung zur Minderung des aerodynamischen Lärms an einem Vorflügel eines Verkehrsflugzeuges
US6974112B2 (en) * 2003-06-17 2005-12-13 Michael Craig Broadbent Deployment system for a moveable wing surface
US20060038088A1 (en) * 2004-08-23 2006-02-23 Dodson Robert T Aircraft wing
DE102004049504A1 (de) * 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7249735B2 (en) * 2005-06-30 2007-07-31 The Boeing Company Translating conduit apparatus for an airplane or equipment
US7635107B2 (en) * 2005-08-09 2009-12-22 The Boeing Company System for aerodynamic flows and associated method
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
DE102005044549B4 (de) * 2005-09-17 2008-04-17 Eads Deutschland Gmbh Flugzeugflügel mit ausfahrbarer Nasenklappe
US7753316B2 (en) * 2007-04-27 2010-07-13 The Boeing Company Deployable flap edge fence
GB0708334D0 (en) * 2007-04-30 2007-06-06 Airbus Uk Ltd Method and apparatus for deploying an auxiliary airfoil
DE102007020870A1 (de) * 2007-05-04 2008-11-13 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
US20140339358A1 (en) * 2007-12-06 2014-11-20 Roller Bearing Company Of America, Inc. Electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices
GB0911016D0 (en) * 2009-06-25 2009-08-12 Airbus Operations Ltd Electrical power transmitting telescopic strut
US8534610B1 (en) * 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
DE102009052641A1 (de) * 2009-11-10 2011-05-12 Airbus Operations Gmbh Hinterkantenklappensystem
GB0920968D0 (en) * 2009-11-27 2010-01-13 Airbus Operations Ltd Trailing edge flap
GB0921487D0 (en) * 2009-12-08 2010-01-20 Airbus Operations Ltd Slat support assembly
DE102009060326A1 (de) * 2009-12-23 2011-06-30 Airbus Operations GmbH, 21129 Hochauftriebssystem für ein Flugzeug
GB201006099D0 (en) * 2010-04-13 2010-05-26 Airbus Operations Ltd Slat support assembly
GB201220885D0 (en) * 2012-11-20 2013-01-02 Airbus Operations Ltd An improved deployment mechanism
EP3241740B1 (fr) * 2016-05-03 2020-08-19 Airbus Operations GmbH Système d'entraînement d'un dispositif de lamelle d'une aile d'avion
US10259566B1 (en) * 2016-06-13 2019-04-16 James Randolph Lawrence Rolling vortex wing slat system and method of use
EP3299278B1 (fr) * 2016-09-23 2020-06-03 Airbus Operations GmbH Dispositif de suivi de bec de bord d'attaque pour une aile d'avion
EP3326909B1 (fr) * 2016-11-23 2019-10-02 Airbus Operations GmbH Assemblage du bec du bord d'attaque
EP3339163A1 (fr) * 2016-12-22 2018-06-27 Airbus Operations GmbH Aile d'avion
EP3395679B1 (fr) * 2017-04-28 2021-09-01 Airbus Operations GmbH Aile d'avion

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4202519A (en) * 1978-09-08 1980-05-13 The Boeing Company Airfoil leading edge slat apparatus
CN101466597A (zh) * 2006-06-14 2009-06-24 波音公司 用于有间隙刚性克鲁格襟翼的连杆机构及相关系统和方法
CN101450712A (zh) * 2007-12-06 2009-06-10 滚动轴承美国公司 用于升力辅助装置的致动系统和其中使用的滚子轴承
EP2272752A2 (fr) * 2009-07-07 2011-01-12 Goodrich Actuation Systems Limited Agencement d'actionneur
CN102834315A (zh) * 2010-03-31 2012-12-19 波音公司 带有可展开机翼前缘元件的低噪音机翼缝翼系统
CN104039647A (zh) * 2011-06-28 2014-09-10 空中客车运作有限责任公司 具有主翼和增升体的机翼及实现调节增升体相对于主翼的运动的方法
CN103448906A (zh) * 2012-05-31 2013-12-18 空中客车营运有限公司 缝翼支撑组件

Also Published As

Publication number Publication date
US11021229B2 (en) 2021-06-01
US20180178900A1 (en) 2018-06-28
EP3339163A1 (fr) 2018-06-27
CN108216578A (zh) 2018-06-29

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